N815SK
Service difficulty reports · 88
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N815SK' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N815SK' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWIA2018070644852Post · corrodedRT FS 280.00 FLOOR POST RBL11.16 P/N CC670-34180 HAS PITTING CORROSION. (C-CHECK) RO: 07/01/2018 REMOVED AND INSTALLED NEW FS 280.00 RT FLOOR POST AT RBL 11.16 IAW SRM.SDR SWIA2018070644851Web · corrodedRT FS 280.00 LOWER WEB IS CORRODED AT DRIP CAP AND CROSSBEAM AREAS. (C-CHECK) RO: 07/01/2018 REMOVED RT FS 280.00 LOWER WEB AND INSTALLED NEW RT FS 280.00 LOWER WEB IAW SRM.SDR SWIA2018070644850Web · corrodedLT FS 280.00 LOWER WEB IS CORRODED AT DRIP CAP AND CROSSBEAM AREAS. (C-CHECK) RO: 07/01/2018 REMOVED LT FS 280.00 LOWER WEB AND INSTALLED LT FS 280.00 LOWER WEB IAW SRM.SDR SWIA2018070644849Door Sill · corrodedRT FLOOR SILL AFT OF FS 280.00 IS CORRODED. (C-CHECK) RO: 07/01/2018 REMOVED & REPLACED THE RT FLOOR SILL FS 280.00 TO FS 319.00 IAW SRM. ALL CHECKS GOOD.SDR SWIA2018070644848Intercostal · corrodedINTERCOSTAL CORRODED AT FS 310 - FS 333 STR 21L. (C-CHECK) RO: 07/01/2018 REMOVED & INSTALLED NEW INTERCOSTAL AT FS 310-FS 333 STR 21 IAW SRM. LEAK CHECK GOOD.SDR SWIA2018070644847Strap · corrodedFS 280.00 CROSSBEAM TOP STRAP LBL 9.0 TO RBL 9.0 IS CORRODED. (C-CHECK) RO: 07/01/2018 REMOVED AND INSTALLED NEW FS 280.00 TOP STRAP P/N CC670-34097-1SB IAW SRM.SDR SWIA2018070644846Crossbeam · corrodedLT FS 280.00 CROSSBEAM HAS CORROSION. (C-CHECK) RO: 07/01/2018 REMOVED AND INSTALLED NEW LT FS 280.00 CROSSBEAM P/N CC670-34094-1 IAW SRM.SDR SWIA2018070644845Crossbeam · corrodedRT FS 280.00 CROSSBEAM IS CORRODED. (C-CHECK) RO: 07/01/2018 REMOVED AND INSTALLED NEW RT FS280.00 CROSSBEAM P/N CC670-34094-4 IAW SRM.SDR SWIA2018070644844Angle · corrodedPAX DOOR SILL ANGLE SHOWS EVIDENCE OF CORROSION BETWEEN FS310.00 & FS349.00. (C-CHECK) RO: 07/01/2018 REPLACED PAX DOOR SURROUND KICK PLATE AND MID CAP ANGLE WITH NEW. P/N: SH670-31875-3S & SH670-31825-7. INSTALLED NEW PAX DOOR KICK PLATE ANGLE AND INSTALLED NSDR SWIA2018070644843Floor Support · corrodedFS 280.00 CENTER COCKPIT FLOOR SUPPORT ANGLE CORRODED. (C-CHECK) RO: 07/01/2018 REMOVED AND INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLE P/N CC670-34095-1SB IAW SRM.SDR SWIA201844128Sensor · out of adjustNOSE DOOR OPEN WARNING MESSAGE AFTER TAKEOFF. ADJUSTED PX31 AND PERFORMED NOSE GEAR SWING IAW AMM. CHECKED GOOD.SDR SWIA201642223Packing · failedGEAR DISAGREE AFTER TAKEOFF AND NWS IN-OP CAUTION MESSAGE. REPACKED NLG STRUT AND PERFORMED FULL STRUT SERVICE AND PERFORMED LANDING GEAR SWINGS. LEAK CHECK AND OPS CHECKED GOOD.SDR SWIA201642070Frame · corrodedAVIONICS BAY LOWER FRAME AT BS 295 CORRODED. INSTALLED A NEW FRAME IAW SRM AND REO. PRESSURIZATION CHECKED GOOD.SDR SWIA201642068Frame · corrodedAVIONICS BAY LOWER FRAME AT BS 333 CORRODED. INSTALLED A NEW FRAME IAW SRM AND REO. PRESSURIZATION CHECK GOOD AT THIS TIME.SDR SWIA201642067Frame · corrodedAVIONICS BAY LOWER FRAME AT BS 349 CORRODED. R & R THE FRAME IAW SRM. PRESSURE CHECKS GOOD AT THIS TIME.SDR SWIA201642072Stringer · corrodedSTRINGER 19R BS 661+90 CORRODED. R & R THE STRINGER IAW SRM.SDR SWIA201642071Intercostal · corrodedINTERCOSTAL IN AVIONICS BAY BS 364 - 349, STR 27L CORRODED. R & R THE INTERCOSTAL IAW SRM. PRESSURE CHECKED GOOD.SDR SWIA201642069Doubler · corrodedTCAS ANTENNA DOUBLER IN AVIONICS BAY CORRODED. R & R TCAS ANTENNA DOUBLER IAW AMM. PRESSURE CHECKED GOOD.SDR SWIA201642066Intercostal · corrodedCORRODED INTERCOSTAL IN AVIONICS BAY BS 364 - 349, STR 27R. R & R THE INTERCOSTAL IAW SRM. PRESSURE CHECKS GOOD AT THIS TIME.SDR SWIA201642065Intercostal · corrodedPAX DOOR FWD INTERCOSTAL CORRODED. R & R IAW SRM. PRESSURE CHECK GOOD.SDR SWIA201540940Skin · dentedRT WING L/E NR 1 SLAT HAS DENT FROM BIRDSTRIKE. DENT IS APPROXIMATELY 3 FT FROM INBD AND 2" FROM BOTTOM OF SLAT. DENT IS APPROX 2.5" IN DIAMETER AND .035" DEEP. RO: 03/27/2015, FILLED DENT IAW REO.SDR SWIA201439666Skin · dentedRT ENGINE COWL IS DENTED OUT OF LIMITS. REPLACED IAW AMM.SDR SWIA201438939Battery Pack · inoperativeFORWARD F/A FLASHLIGHT DOES NOT BLINK. R & R FWD F/A FLASHLIGHT BATTERY, OPS CHECKED GOOD IAW AMM.SDR SWIA201437715Bulb · inoperativeRT NR 3 OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RT AFT OVERWING SECTION EMERGENCY LIGHT BULB AND CRACKED LENS COVER IAW AMM.SDR SWIA201437626Seat Track · corrodedRIGHT FLOOR SEAT RAIL AT FS477.00 THRU 573.00 CORRODED. C-CHECK, R & R RT FLOOR SEAT RAIL AT FS477.00 - FS 573.00 IAW AMM.SDR SWIA201437621Angle · corrodedPAX DOOR MID-CAP ANGLE HAS CORROSION. C-CHECK, REPLACED NEW PAX DOOR MID CAP ANGLE, PN SH670-31825-7 IAW SRM.SDR SWIA201437622Structure · chafedBOTTOM OF FUSELAGE CHAFED AT APPROXIMATELY FS969, STGR27, C-CHECK, BLENDED CHAFE ON FUSELAGE A FS 969, STR 27 IAW REO.SDR SWIA201437629Striker · dentedPASSENGER DOOR EXTERNAL SURROUND STRUCTURE AT FS 310, UPPER SECTION HAS A DENT. C-CHECK, REPAIRED PASSENGER DOOR SURROUND SEAL STRIKER IAW REO.SDR SWIA201437628Striker · dentedPASSENGER DOOR EXTERIOR SURROUND STRUCTURE AT FS 349, UPPER SECTION HAS DENT. C-CHECK, REPAIRED PASSENGER DOOR SURROUND SEAL STRIKER IAW REO.SDR SWIA201437627Seat Track · corrodedSIDE SEAT RAIL HAS CORROSION AT APPROXIMATELY FS 746.00 ON STG 15L. C-CHECK, REPAIRED SIDE SEAT RAIL AT APPROXIMATELY FS 746.00 ON STG 15L. LARGEST MATERIAL LOSS FOUND AT LOACTION "Z". STARTING GAP- 0.420", REMAINING GAP- 0.459", MATERIAL REMOVED- 0.039", WISDR SWIA201437625Seat Track · corrodedLT SIDE FLOOR SEAT TRACK HAS CORROSION AT APPROXIMATELY FS 612.00 ON LBL 9.00. C-CHECK, REPAIRED LT SIDE FLOOR SEAT TRACK AT APPROXIMATELY FS 612.00 ON LBL 9.00. LARGEST MATERIAL LOSS FOUND AT LOCATION "Z". STARTING GAP- 0.420", REMAINING GAP- 0.430", MATERISDR SWIA201437624Seat Track · corrodedLEFT SIDE FLOOR SEAT TRACK HAS CORROSION AT APPROXIMATELY FS 661.00 + 82.00 ON LBL 9.00. C-CHECK, REPAIRED LT SIDE FLOOR SEAT TRACK AT APPROXIMATELY FS 661.00 + 82.00 ON LBL 9.00. LARGEST MATERIAL LOSS FOUND AT LOCATION "Z". STARTING GAP- 0.420", REMAININGSDR SWIA201437623Seat Track · corrodedLT SIDE FLOOR SEAT TRACK HAS CORROSION AT APPROXIMATELY FS 693.00 ON LBL 9.00. C-CHECK, REPAIRED LT SIDE FLOOR SEAT TRACK AT APPROXIMATELY FS 693.00 ON LBL 9.00. LARGEST MATERIAL LOSS FOUND AT LOCATION "Z". STARTING GAP- 0.420", REMAINING GAP- 0.429", MATERSDR SWIA201437638Support Arm · chafedFWD BAGGAGE BAY DOOR FWD LOWER SUPPORT ARM CHAFED ON TOP SIDE. C-CHECK, BLENDED CHAFE ON FWD BAGGAGE BAY DOOR FWD LOWER SUPPORT ARM TOP SIDE IAW SRM AND STS EA.SDR SWIA201437637Rod · chafedRIGHT INBD FLAP VANE ACTUATOR ROD UNDER ACCESS PANEL 684AB CHAFED ON CHROME SURFACE. C-CHECK, BLENDED CHAFE ON RT INBD FLAP VANE ACTUATOR ROD UNDER PANEL 684AB, AND FOUND TO BE WITHIN LIMITS IAW REO.SDR SWIA201437636Rod · chafedRIGHT INBD FLAP VANE ACTUATOR ROD UNDER ACCESS PANEL 684CB CHAFED ON CHROME SURFACE. C-CHECK, BLENDED CHAFE ON RT INBD FLAP VANE ACTUATOR ROD UNDER PANEL 684CB, AND FOUND TO BE WITHIN LIMITS, IAW REO.SDR SWIA201437635Rod · chafedRT INBD FLAP VANE ACTUATOR ROD UNDER ACCESS PANEL 684DB CHAFED ON CHROME SURFACE. C-CHECK, BLENDED CHAFE ON RT INBD FLAP VANE ACTUATOR ROD UNDER PANEL 684DB, AND FOUND TO BE WITHIN LIMITS IAW REO AND AMM.SDR SWIA201437634Lever · chafedPAX DOOR FWD PULL-IN LEVER CHAFED. C-CHECK, BLENDED CHAFED AREA, REQUESTED NDT FOR CRACK CHECK NO DEFECTS WERE NOTED. ORIGINAL MATERIAL THICKNESS WAS 1.700". AFTER RE-WORK MATERIAL THICKNESS IS 1.665". A TOTAL LOSS OF .035. TOTAL ALLOWABLE LOSS IS .050". SDR SWIA201437633Structure · corrodedPAX DOOR FWD LOWER CAM LATCH HAS CORROSION UNDERNEATH. C-CHECK, REMOVED CORROSION FROM UNDERNEATH FWD LOWER CAM LATCH OF PAX DOOR IAW SRM.SDR SWIA201437632Attach Bracket · crackedPAX DOOR AFT ANGLE BRACKET CRACKED NEXT TO PULL-IN CABLE ASSIST WHEEL BRACKET. C-CHECK, REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO.SDR SWIA201437631Support · chafedPAX DOOR SUPPORT WHEEL CHAFED. C-CHECK, BLENDED CHAFE ON PAX DOOR SUPPORT WHEEL IAW STS EA.SDR SWIA201437630Support · chafedPAX DOOR AFT HAND RAIL OTBD SUPPORT ARM CHAFED FROM PAX DOOR SUPPORT WHEEL. C-CHECK, BLENDED CHAFE ON PAX DOOR AFT HANDRAIL OTBD SUPPORT ARM ORIGINAL MATERIAL THICKNESS .083" REMAINING MATERIAL THICKNESS .078" MATERIAL LOSS OF .005" IS WITHIN LIMITS IAW STS SDR SWIA201436677Engine · vibrationAT FL 380, ROUGHLY 30 SECONDS AFTER REDUCING TL TO CRUISE SETTING A SIGNIFICANT VIBRATION WAS FELT THROUGHOUT THE AIRFRAME. REPLACED LT ENGINE ASSY IAW AMM.SDR SWIA201334963Light · inoperativeNR 1 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#4503 RELAMPED.SDR SWIA201334795Light · inoperativeNR 5 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#4693 RELAMPED.SDR SWIA201333484Lamp · burned outOVERHEAD EMERGENCY LIGHT AT ROW 14 BURNED OUT, REPLACED LAMPS.SDR SWIA201333173Light · inoperativeEMERGENCY LIGHT AT ROW 8 IS BURNED OUT. (FLT 4661) RELAMPED EMERGENCY LIGHT.SDR SWIA201332690Light · inoperativeTHIRD FROM REAR OVERHEAD CABIN EMERGENCY LIGHT IS BURNED OUT. (FLT 4618) RELAMPED EMERGENCY LIGHT.SDR SWIA201231598Light · inoperativeOVERWING EXIT ROW LIGHT PARTIALLY INOPERATIVE AT ROW 13 ON THE RIGHT SIDE. (FLT 4618) RELAMPED EMERGENCY LIGHTS AT FOOT LEVEL AT ROW 13C/D SIDE IN REFERENCE TO AMM.SDR SWIA201231069Light · inoperativeAFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4452) RELAMPED EMERGENCY LIGHT.
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